A fnite element parametric modeling technique of aircraft wing structures

作     者：Tang Jiapeng Xi Ping Zhang Baoyuan Hu Bifu 

作者机构：School of Mechanical Engineering and AutomationBeihang University School of Mechatronic EngineeringNorth University of China 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：2013年第26卷第5期

页      面：1202-1210页

核心收录：

学科分类：08[工学] 082501[工学-飞行器设计] 0825[工学-航空宇航科学与技术] 

基　　金：supported by the National Natural Science Foundation (No.51075021) 

主　　题：Finite element model Geometric mesh model Knowledge Parametric modeling Skeleton model Template Wing 

摘      要：A finite element parametric modeling method of aircraft wing structures is proposed in this paper because of time-consuming characteristics of finite element analysis pre-processing. The main research is positioned during the preliminary design phase of aircraft structures. A knowledge- driven system of fast finite element modeling is built. Based on this method, employing a template parametric technique, knowledge including design methods, rules, and expert experience in the process of modeling is encapsulated and a finite element model is established automatically, which greatly improves the speed, accuracy, and standardization degree of modeling. Skeleton model, geometric mesh model, and finite element model including finite element mesh and property data are established on parametric description and automatic update. The outcomes of research show that the method settles a series of problems of parameter association and model update in the process of finite element modeling which establishes a key technical basis for finite element parametric analysis and optimization design.